发明名称 THRUST DEFLECTING DEVICE AND AIRCRAFT ENGINE
摘要 A thrust deflecting device for deflecting a thrust stream is disclosed, which includes a flap system having a plurality of deflecting flaps, each of which is pivotable around its yaw axis, the flap system being situated between parallel control surfaces such as baffle plates which, together with the flap system, form a box structure, which is pivotable around a pivot axis running in the direction of the transverse axis for the purpose of deflecting the thrust stream in the pitch direction, an aircraft engine also being disclosed.
申请公布号 US2015226155(A1) 申请公布日期 2015.08.13
申请号 US201414299727 申请日期 2014.06.09
申请人 MTU Aero Engines AG 发明人 Klingels Hermann;Klaen Stephan;Scherer Christian;Vogel Uwe
分类号 F02K1/00;F02K1/80;B64D33/04 主分类号 F02K1/00
代理机构 代理人
主权项 1. A thrust deflecting device for deflecting a thrust stream of an aircraft engine, the thrust deflecting device comprising: a housing; a flap system having a plurality of deflecting flaps, each deflecting flap pivotable around a yaw axis extending orthogonally with respect to a transverse axis of the thrust deflecting device; and two parallel baffle plates extending downstream from the housing, the flap system situated between the two parallel baffle plates, the two parallel baffle plates together with the flap system being pivotable around a pivot axis running in the direction of the transverse axis for the purpose of deflecting the thrust stream in a pitch direction.
地址 Muenchen DE